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Experimental investigation of effect of spike- tip and cowl-lip blunting on the internal performance of a two-cone cylindrical-cowl inlet at mach number 4.95

机译：尖头和整流罩钝化对马赫数为4.95的双锥圆柱罩进口内部性能影响的实验研究

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作者
Weston, K. C.;
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年度 1958
页码 1-18
总页数 18
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
COWLINGS; ENGINE INLETS; SUPERSONIC SPEED; AERODYNAMIC CHARACTERISTICS; AERODYNAMIC CONFIGURATIONS; SYSTEMS ENGINEERING;

机译：整流罩;发动机进气;超音速;空气动力学特征;空气动力学配置;系统工程;

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1. Flow characteristics of hypersonic inlets with different cowl-lip blunting methods [J] . LU HongBo, YUE LianJie, CHANG XinYu 中国科学:物理学力学天文学（英文版） . 2014,第004期

机译：不同罩唇套装的超声口腔流动特性
2. Investigation of aerodynamic heating in V-shaped cowl-lip of the inward turning inlet [J] . Meng Zewei, Fan Xiaoqiang, Xiong Bing, Proceedings of the Institution of Mechanical Engineers . 2019,第8期

机译：向内进气口V形前缘的空气动力加热研究
3. Investigation of aerodynamic heating in V-shaped cowl-lip of the inward turning inlet [J] . Meng Zewei, Fan Xiaoqiang, Xiong Bing, Proceedings of the Institution of Mechanical Engineers . 2019,第8期

机译：向内转动入口V形罩唇缘的空气动力学加热研究
4. Experimental Investigation on the Influence of Yaw Angle on the Inlet Performance at Mach 7 [C] . O. Hohn, A. GÃ AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition . 2010

机译：偏航角对7马赫进气口性能影响的实验研究
5. Experimental pressure and heat transfer investigation over a "directed-energy air spike" inlet at flow mach numbers of 10 to 20, stagnation temperature of 1000 K, and arc powers up to 127 KW. [D] . Toro, Paulo Gilberto de Paula. 1998

机译：在流量为10至20的马赫数，停滞温度为1000 K，电弧功率高达127 KW的“定向能空气尖峰”入口上进行实验压力和传热研究。
6. Experimental Investigation on Graphene Oxide/SrCl2·6H2O Modified CaCl2·6H2O and the Resulting Thermal Performances [O] . Zhiyang Jin, Yuanyuan Tian, Xiaoxiao Xu, 2018

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7. Reynolds Number and Cowl Position Effects for a Generic Sidewall Compression Scramjet Inlet at Mach 10: A Computational and Experimental Investigation [O] . Holland Scott D. 1992

机译：通用侧壁压缩超燃冲压发动机进气口在10马赫时的雷诺数和风帽位置影响：计算和实验研究
8. Experimental Investigation of the Performance of a Mach-2.7 Two-DimensionalBifurcated Duct Inlet with 30 Percent Internal Contraction [R] . Wasserbauer, J. F., Meleason, E. T., Burstadt, P. L. 1996

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Experimental investigation of effect of spike- tip and cowl-lip blunting on the internal performance of a two-cone cylindrical-cowl inlet at mach number 4.95

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